N171HQ
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
55 reports on file, 2010-02-23 – 2014-08-14.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 14,285 hrs · 9,181 cycles
DURING EXIT CHECK, L2 DOOR SURROUND EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE R & R EMERGENCY BATTERY IAW AMM AND OPS CHECKED GOOD.
Part: CONNECTOR — CORRODED (TAXI LIGHT) · corrosion level 2 · airframe 14,285 hrs · 9,181 cycles
DURING HEAVY CHECK, CONNECTOR P1026 ON NLG INSIDE FOUND CORRODED. MX R & R NLG TAXI LIGHT HARNESS IAW AMM 32-21-01, CMM 32-21-01.
Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 14,285 hrs · 9,181 cycles
DURING HEAVY CHECK, CF3 LT INBD SEAT TRACK BEAM FWD OF FRAME 85 IS CORRODED. MX R & R CF3 LT INBD SEAT TRACK BEAM FWD OF FRAME 85 IAW SRM 51-40-02, 51-43-01.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 14,285 hrs · 9,181 cycles
DURING HEAVY CHECK, LT SEAT TRACK EXTENSION DOUBLER AT FRAME 85 IS CORRODED. MX R & R LT SEAT TRACK EXTENSION DOUBLER AT FRAME 85 IAW SRM 51-40-02,
Part: SEAL REST — CORRODED (FWD CARGO DOOR) · corrosion level 2 · airframe 14,285 hrs · 9,181 cycles
DURING HEAVY CHECK, FWD CARGO DOOR LOWER SEAL DEPRESSOR HAS SEVERAL SPOTS OF CORROSION. MX R & R FWD CARGO DOOR LOWER SEAL DEPRESSOR IAW SRM 51-41-01,51-41-02.
Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 14,285 hrs · 9,181 cycles
DURING HEAVY CHECK, RT SEAT TRACK EXTENSION DOUBLER AT FRAME 85 FWD OF FRAME 86 IS CORRODED. MX R & R RT SEAT TRACK EXTENSION DOUBLER AT FRAME 85 FWD OF FRAME 86 IAW SRM 51-40-02.
Part: BRACKET — CORRODED (ZONE 100) · corrosion level 2 · airframe 14,285 hrs · 9,181 cycles
DURING HEAVY CHECK, BRACKET AROUND WASTE BOX INSIDE OF ACFT AT 9 O`CLOCK POSITION IS CORRODED. MX R & R BRACKET IAW SRM 51-43-01.
Part: NUT PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 14,285 hrs · 9,181 cycles
DURING HEAVY CHECK, WASTE BOX NUT PLATES ARE CORRODED. INSTALLED FASTENERS IN WASTE BOX IAW SB 190-53-0056.
Part: FIREWALL — CRACKED (ZONE 100) · airframe 14,285 hrs · 9,181 cycles
DURING HEAVY CHECK, APU FIRE WALL AT TOP AND BOTTOM OF 351BZ IS CRACKED. MAINTENANCE TRIMMED OUT CRACKS IAW SRM 53-31-21.
Part: SCREW — CORRODED (GIRT BAR) · corrosion level 2 · airframe 14,285 hrs · 9,181 cycles
DURING HEAVY CHECK, WAS REPORTED THAT L2 DOOR EMERGENCY SLIDE GIRT BAR CABLE CLEVIS AT GIRT BAR END HARDWARE IS CORRODED. MX R & R L2 DOOR EMERGENCY SLIDE GIRT BAR CABLE CLEVIS AT GIRT BAR END HARDWARE IAW AMM 52-12-40, PN NAS 1154-10D, SCREW.
Part: BRACKET — CRACKED (NLG WW) · airframe 14,285 hrs · 9,181 cycles
DURING HEAVY CHECK, NLG STEERING MANIFOLD BRACKET IS CRACKED. MX R & R NLG STEERING MANIFOLD BRACKET IAW SRM 51-40-02, 51-43-03 REFER TO CONTINUATION CARD VP-026804-2014/161 C1-C2 FOR WORK DETAILS. PN 170-10788-401, SUPPORT ASSY.
Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 14,285 hrs · 9,181 cycles
DURING HEAVY CHECK, LEFT EMERGENCY RAM AIR VALVE SUPPORT BRACKETS ARE CRACKED. MAINTENANCE R & R LT EMERGENCY RAM AIR VALVE SUPPORT BRACKETS IAW SRM 51-40-02, 51-41-01 SEE CONTINUATION CARD 162C1 FOR WORK DETAILS. PN 190-27133-003, SUPPORT.
Part: PAN — CRACKED (SEAT 14L) · airframe 14,285 hrs · 9,181 cycles
DURING HEAVY CHECK, SEAT 14L PAN IS CRACKED. MX REMOVED AND REPLACED SEAT PAN IAW SRM 51-42-00.
Part: DOOR — MISINSTALLED (EMERGENCY EXIT) · airframe 13,934 hrs · 8,903 cycles
CREW RECEIVED A RT OVERWING EMERGENCY DOOR OPEN INDICATION. RAN QRH, DECLARED AN EMERGENCY AND DIVERTED. LANDED AND TAXIED TO GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE RT OVERWING EMERGENCY DOOR NOT SEATED PROPERLY. MAINTENANCE RESEATED DOOR AND PERFORMED PRESSURE CHECK IAW AMM AND OPS CHECKED GOOD. ACFT IS GOOD FOR SERVICE.
Earlier reports · 2010–2013 · 41 reports
2013
Part: FLASHLIGHT — DIM (AFT CABIN) · airframe 13,636 hrs · 8,754 cycles
CREW REPORTED THAT THE AFT F/A FLASHLIGHT WAS NOT BRIGHT. MAINTENANCE R & R THE AFT RT F/A FLASHLIGHT IAW AMM AND OPS CHECKED GOOD.
Part: GIRT BAR — DIRTY (R1 DOOR) · airframe 13,320 hrs · 8,602 cycles
CREW REPORTED THAT THE R1 DOOR WILL CLOSE BUT WILL NOT ARM. MX CLEANED GIRT BAR AREA AND PERFORMED OPS CHECK OF THE R1 DOOR IAW AMM AND OPS CHECKED GOOD. ACFT IS GOOD FOR SERVICE.
Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 13,123 hrs · 8,495 cycles
CREW REPORTED THAT THE CAPTAINS FLASHLIGHT DOES NOT WORK. MX R & R FLASHLIGHT BATTERIES IAW AMM AN OPS CHECKED GOOD.
Part: BRAKE ASSY — OVERHEATED (MLG) · airframe 13,103 hrs · 8,484 cycles
CREW RECEIVED A LANDING GEAR NO DISPATCH MESSAGE ON ROLLOUT AFTER LANDING. SHORTLY AFTER THE BRAKE OVERHEAT MESSAGE APPEARED AND THE LT OTBD BRAKE TEMP PEAKED AT 465 DEGREES WHILE THE LT INBD BRAKE TEMP WAS ABOUT 88. CREW STOPPED ACFT TO ALLOW BRAKE TO COOL AND TOWER CALLED FIRE TRUCKS TO INVESTIGATE. AFTER ALLOWING THE BRAKES TO COOL THE CREW TAXIED TO THE GATE WITHOUT INCIDENT. MX FOUND THE BRAKE GRABBING AND R & R IAW AMM. ACFT IS GOOD FOR SERVICE.
Part: FLASHLIGHT — DEFECTIVE (CABIN) · airframe 12,754 hrs · 8,292 cycles
CREW REPORTED THAT THE FORWARD F/A FLASHLIGHT IS DIM. MX R & R FLASHLIGHT IAW AMM AND OPS CHECKED GOOD.
Part: SLIDE — UNWANTED DEPLOY (L1 DOOR) · airframe 12,654 hrs · 8,232 cycles
CREW REPORTED THAT THEY MAY HAVE INADVERTENTLY DEPLOYED THE L1 DOOR SLIDE. MX CONFIRMED IT WAS DEPLOYED AND REPLACED IAW AMM. OPS CHECKED GOOD.
Part: SENSOR — DEFECTIVE (LE SLAT) · airframe 12,377 hrs · 8,083 cycles
CREW RECEIVED A SLAT FAIL MESSAGE DURING CLIMB FROM DCA - OMA. CREW FOLLOWED QRH AND MESSAGE DID NOT CLEAR. AFTER CONSULTING WITH MAINTENANCE, CREW ELECTED TO CONTINUE TO OMA. ATC DECLARED AN EMERGENCY AND EMERGENCY VEHICLES WERE ROLLED AS A PRECAUTION. CREW LANDED IN OMA WITHOUT INCIDENT AND TAXIED TO GATE WITHOUT ISSUE. MAINTENANCE FOUND THE SLAT SKEW SENSOR AND 3/4 RIGHT HARNESS BAD. MAINTENANCE REPLACED BOTH PER EMB AMM AND OPS CHECKED GOOD.
Part: SHUTOFF VALVE — LEAKING (BLEED AIR SYS) · airframe 12,320 hrs · 8,050 cycles
WHILE AT CRUISE ALTITUDE WITH BLEED 2 ON MEL, CREW RECEIVED A BLEED 1 LEAK MESSAGE. CREW FOLLOWED QRH ITEMS WITH NO RESULTS AND CABIN ALTITUDE STARTED TO SLOWLY RISE. CREW COMMENCED AN EMERGENCY DESCENT TO 10,000 FEET AND DECLARED AN EMERGENCY. BY THIS TIME THE CABIN ALTITUDE WAS BACK TO A NORMAL SITUATION AND CREW ELECTED TO BURN OFF FUEL TO AVOID AN OVER WEIGHT LANDING. CREW LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 NAPRSOV LEAKING AND REMOVED AND REPLACED THE NR 1 NAPRSOV AND THE NR 2 NAPRSOV GASKET PER EMB AMM AND OPS CHECKED GOOD.
Part: BRAKE — SEIZED (MLG) · airframe 12,164 hrs · 7,965 cycles
CREW REPORTED THAT UPON LANDING THEY NEEDED TO APPLY POWER INSTEAD OF BRAKES TO MAKE THE FIRST HIGH SPEED TAXIWAY. THEY IMMEDIATELY RECEIVED A LANDING GEAR TEMPERATURE EXCEEDANCE, BRAKE OVERHEAT & LANDING GEAR NO DISPATCH MESSAGE. LEFT OUTBOARD BRAKE TEMP SPIKED AT 785 DEGREES. CREW SLOWLY TAXIED TO THE GATE WITH EMERGENCY EQUIPMENT FOLLOWING. PASSENGERS EXITED NORMALLY WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 BRAKE SEIZED AND TIRE FLAT SPOTTED, BUT NOT DEFLATED. MAINTENANCE REPLACED NR 1 BRAKE AND NR 1 BRAKE HOSE PER EMB AMM AND OPS CHECKED GOOD.
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 12,023 hrs · 7,882 cycles
CREW DISCOVERED AFT FLIGHT ATTENDANT FLASHLIGHT INOP. MAINTENANCE REMOVED AND REPLACED AFT FLIGHT ATTENDANT FLASHLIGHT PER EMB AMM 33-51-01. OPS CHECKED GOOD.
Part: FUSE — INOPERATIVE (PARKING BRAKE) · airframe 11,775 hrs · 7,699 cycles
ON APPROACH, CREW RECEIVED PARKING BRAKE NOT RELEASED MESSAGE. EMERGENCY VEHICLES STANDING BY, CREW LANDED AND TAXIED TO GATE WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED PARKING BRAKE FUSE PER EMB AMM AND OPS CHECKED GOOD.
2012
Part: DOOR — DIRTY (CABIN) · airframe 11,107 hrs · 7,178 cycles
CREW REPORTED THE LATCH ON THE FWD EMERGENCY EQUIPMENT DOOR IS STICKY. MAINTENANCE CLEANED AND LUBED THE FORWARD CABIN STORAGE COMPARTMENT LATCH PER EMB 190 AMM 20-10-0.
Part: RIB — CRACKED (LT WING) · airframe 10,796 hrs · 6,925 cycles
WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE UPPER FLANGE OF LEFT WING RIB 10 CRACKED. MAINTENANCE REPAIRED THE RIB 10 LEFT WING IAW EMB SB 190-57-0026 REV 1. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.
Part: RIB — CRACKED (RT WING) · airframe 10,796 hrs · 6,925 cycles
WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE UPPER FLANGE RIGHT WING RIB 10 CRACKED. MAINTENANCE REPAIRED THE RIGHT WING RIB 10 IAW EMB SB 190-57-0026. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.
Part: UPPER SHEET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,796 hrs · 6,925 cycles
WHILE A/C WAS IN FOR HEAVY CHECK FOUND STRAP ON RIGHT Z-BEAM HAS CORROSION BETWEEN FR 85-86. MX REMOVED AND REPLACED CORRODED STRAP (UPPER SHEET) IAW EMB 190 SRM 51-40-02, 51-43-03, 51-41-01. P/N 170-86101-001. A/C REMAINS IN CMH FOR HEAVY CHECK COMPLETION.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,796 hrs · 6,925 cycles
WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND INBOARD LEFT CF3 SEAT TRACK AT FRAME 84 CORRODED. MAINTENANCE REMOVED AND REPLACED SEAT TRACK INBOARD LEFT CF3 AT FRAME 84 IAW EMB 190 SRM 51-43-01, 51-43-02, AND 51-43-04. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.
Part: DOOR FRAME — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 10,796 hrs · 6,925 cycles
WHILE A/C WAS IN FOR HEAVY CHECK FOUND FWD CARGO DOOR AFT LOWER FRAME HAS SPOTS OF CORROSION. MX REMOVED AND REPLACED OLD REST IAW EMB 190 AMM 20-10-01, EMB 190SRM51-40-02. PN 170-66803-402. A/C REMAINS IN CMH FOR HEAVY CHECK COMPLETION.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,796 hrs · 6,925 cycles
WHILE A/C WAS IN FOR HEAVY CHECK FOUND CF3 RIGHT CENTER SEAT TRACK HAS CORROSION AT FR 85. MX REMOVED AND REPLACED CF3 RIGHT CENTER SEAT TRACK IAW EMB 190 SRM 51-41-02, 51-43-01, 51-43-02, 51-41-01, 51-43-04, 51-23-06, 51-23-00. P/N 170-86082-005. A/C REMAINS IN CMH FOR HEAVY CHECK COMPLETION.
Part: HINGE — CORRODED (WASTE BOX) · corrosion level 2 · airframe 10,796 hrs · 6,925 cycles
WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE WASTE BOX DOOR HINGE HALF CORRODED. MAINTENANCE REMOVED AND REPLACED THE WASTE BOX DOOR HINGE HALF IAW EMB 190 SRM 51-41-02, AND 51-43-02.
Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,796 hrs · 6,925 cycles
WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE CF3 LEFT OUTBOARD SHEAR PLATE AT FRAME 87 CORRODED. MAINTENANCE REMOVED AND REPLACED THE CF3 LEFT OUTBOARD SHEAR PLATE AT FRAME 87 IAW EMB 190 SRM 51-42-01, 51-42-02, AND 51-43-01. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.
Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,796 hrs · 6,925 cycles
WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE CF3 RIGHT OUTBOARD SHEAR PLATE CORRODED AT FRAME 87. MAINTENANCE REMOVED AND REPLACED THE CF3 RIGHT OUTBOARD SHEAR PLATE AT FRAME 87 IAW EMB 190 SRM 51-42-01, 51-42-02, AND 51-43-01. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.
Part: HINGE — CORRODED (WASTE BOX) · corrosion level 2 · airframe 10,796 hrs · 6,925 cycles
WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE WASTE BOX DOOR HINGE CORRODED. MAINTENANCE REMOVED AND REPLACED THE WASTE BOX HALF HINGE IAW EMB 190 SRM 51-41-02 AND 51-43-02. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.
Part: UPPER SHEET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,796 hrs · 6,925 cycles
WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE CF3 LEFT CENTER UPPER SHEET CORRODED AT FRAME 87. MAINTENANCE REMOVED AND REPLACED THE CF3 LEFT CENTER UPPER SHEET IAW EMB 190 SRM 51-41-01. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.
Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,796 hrs · 6,925 cycles
WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE CF3 RIGHT OUTBOARD SHEAR PLATE CORRODED FRAME 84. MAINTENANCE REMOVED AND REPLACED CF3 RIGHT OUTBOARD SHEAR PLATE IAW EMB 190 SRM 51-41-02, 51-42-02, AND 51-43-02. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.
Part: HINGE PIN — CORRODED (WASTE BOX) · corrosion level 2 · airframe 10,796 hrs · 6,925 cycles
WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE WASTE BOX DOOR HINGE PIN CORRODED. MAINTENANCE REMOVED AND REPLACED THE WASTE BOX DOOR HINGE PIN IAW EMB 190 SRM 51-41-02, AND 51-43-02. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,796 hrs · 6,925 cycles
WHILE A/C WAS IN FOR HEAVY CHECK FOUND FWD FUSELAGE RIGHT SEAT TRACK HAS MULTIPLE SPOTS OF CORROSION BETWEEN FR 12 AND FR 17. MX REMOVED AND REPLACED FWD FUSELAGE RIGHT SEAT TRACK IAW EMB 190 SRM 51-40-01, 51-23-06. A/C REMAINS IN CMH FOR HEAVY CHECK COMPLETION.
2011
Part: FLAP — MALFUNCTIONED (L1 DOOR) · airframe 9,038 hrs · 5,804 cycles
CREW REPORTED L-1 DOOR VENT FLAP WASN'T CLOSING ALL OF THE WAY. MAINTENANCE INSPECTED L-1 DOOR AND PERFORMED OPS CHECKS ALL PER EMB AMM, NO DEFECTS NOTED.
Part: SHUTOFF VALVE — FAILED (BLEED AIR SYS) · airframe 8,953 hrs · 5,744 cycles
CREW REPORTED BLEED 1 LEAK MSG DURING CLIMB WHILE BLEED 2 WAS ON MEL. CREW DECLARED AN EMERGENCY AND DIVERTED TO PHL, AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RT HPSOV PER EMB AMM, AND PERFORMED HIGH ENGINE RUNS AND REPORTED BOTH BLEED SYSTEMS WERE OPERATING NORMALLY. A/C WAS THEN RETURNED TO SERVICE.
Part: UNKNOWN — MALFUNCTIONED (LE SLAT) · airframe 8,926 hrs · 5,731 cycles
CREW REPORTED SLAT FAIL ON APPROACH INTO MKE. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT INTO MKE. MAINTENANCE TROUBLESHOT PER EMB AMM, AND REPORTED NO DEFECTS NOTED. THE A/C WAS THEN RETURNED TO SERVICE.
Part: SLIDE — DEFECTIVE (L1 DOOR) · airframe 7,929 hrs · 5,120 cycles
MAINTENANCE REPORTED L-1 DOOR SLIDE FAILED TO PROPERLY DEPLOY DURING FUNCTIONAL CHECK. MAINTENANCE REMOVED AND THE L-1 DOOR EMERG EVAC SLIDE PER EMB AMM.
Part: PIN — DISLODGED (L1 DOOR) · airframe 6,436 hrs · 4,384 cycles
CREW REPORTED L-1 DOOR RETAIN PIN WAS DISLODGED. MAINTENANCE INSERTED LANYARD PIN PER EMB AMM, AND PERFORMED OPS CHECKS OF L-1 DOOR.
Part: UNKNOWN — UNKNOWN (L1 DOOR) · airframe 5,987 hrs · 4,150 cycles
CREW REPORTED THE L-1 DOOR GIRT BAR WASN'T SHOWING FULL INDICATION. MAINTENANCE PLACED ON MEL 52-70-01-4.
2010
Part: BELLCRANK — DEFECTIVE (L1 DOOR) · airframe 5,974 hrs · 4,142 cycles
CREW REPORTED L-1 DOOR WOULDN'T DISARM. MAINTENANCE TROUBLESHOT AND REPLACED THE L-1 BELLCRANK ASSEMBLY PER EMB AMM, AND PERFORMED OPS CHECK OF L-1 DOOR.
Part: PIN — OUT OF POSITION (L1 DOOR) · airframe 5,752 hrs · 4,021 cycles
RAMP REPORTED AN L1 BUSTLE STRING HANGING DOWN. MX RE-INSTALLED PIN PER EMB AMM.
Part: GIRT BAR — UNSECURE (L1 DOOR) · airframe 5,747 hrs · 4,018 cycles
CREW REPORTS L1 DOOR WILL NOT ARM. MX RE-SECURED GIRT BAR PER EMB AMM OPS CHECK GOOD.
Part: GIRT BAR — UNSECURE (L1 DOOR) · airframe 5,720 hrs · 4,003 cycles
CREW REPORTED THE L-1 DOOR WOULDN'T ARM. MAINTENANCE RE-SECURED THE L-1 DOOR GIRT BAR PER EMB AMM, OPS CHECK GOOD.
Part: WINDOW — OUT OF POSITION (CABIN) · airframe 5,333 hrs · 3,774 cycles
CREW REPORTED RT OWE SHOWS OPEN IN FLIGHT. MAINTENANCE RESET WINDOW IN DETENT PER EMB AMM, AND MSG CLEARED. A/C WAS THEN RELEASED BACK INTO SERVICE.
Part: DOOR — UNSECURE (EMERGENCY EXIT) · airframe 5,045 hrs · 3,613 cycles
CREW REPORTED AT FL320 RT WINDOW EXIT MSG SHOWED OPEN, MSG WENT AWAY BELOW FL180. NO EMERGENCY DECLARED AND LANDED WITHOUT INCIDENT AT MCI. MAINTENANCE SECURED RT EMERGENCY OVERWING EXIT PER EMB AMM, OPS CHECK GOOD.
Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 4,855 hrs · 3,512 cycles
CREW REPORTED RT EMERGENCY DOOR OPEN MSG IN FLIGHT, NO EMERGENCY WAS DECLARED AND THE A/C LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED RT EMERGENCY EXIT, INSPECTED THE SEAL AND LATCH PER EMB AMM AND RE-INSTALLED EXIT PER EMB AMM, NO FAULTS FOUND.
Part: GIRT BAR — DETACHED (L1 DOOR) · airframe 4,592 hrs · 3,366 cycles
CREW REPORTED L-1 DOOR WOULDN'T OPEN. MAINTENANCE TROUBLESHOT AND RE-ATTACHED THE GIRT BAR PER EMB AMM. A/C WAS THEN RETURNED TO SERVICE.
Part: DUCT — DAMAGED (AC BAY) · airframe 3,558 hrs · 2,798 cycles
CREW REPORTED BURNING SMELL IN CABIN DURING CLIMBOUT OF DEN. CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD AT DEN, AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT TO TROUBLESHOOT, AND FOUND THE DUCTING OF PACK 2 DAMAGED. MAINTENANCE SECURED THE DUCTS AND PLACED THE PACK NR 2 ON MEL 21-51-00-1. THE A/C WAS THEN RETURNED TO SERVICE.